swisspilot
Well-Known Member
Well flight training here in Brazil is changing a lot, many new private schools are opening and the old govt run flight schools are getting neglected, some are in really bad shape. Here in Brazil flight training is usually provided by Flying Clubs with govt owned airplanes, for basic training they are using the Aeroboero AB115 (Argentinian made all metal taildragger http://www.aero-boero.com.ar/) for IFR the Piper Turbo Arrow IV and some Senecas for multi, some also have the AB180 for towing gliders.
Many Clubs are replacing now most of their AB115 with C150s and C152s, all over Brazil there are about 450 units, and seems now you can buy one for about 17K dollars..
General characteristics
Crew: 1
Capacity: 2 passengers
Length: 7.27 m (23 ft 10¼ in)
Wingspan: 10.72 m (35 ft 2 in)
Height: 2.10 m (6 ft 10½ in)
Wing area: 16.5 m² (177 ft²)
Empty weight: 530 kg (1,168 lb)
Max takeoff weight: 770 kg (1,697 lb)
Powerplant: 1× Textron Lycoming O-235-C2A four cylinder, air-cooled, horizontally-opposed, 85.5 kW (115 hp) at 2400 RPM
Performance
Maximum speed: 220 km/h (119 knots, 137 mph) at sea level
Cruise speed: 145 km/h (75 knots, 90 mph) (normal cruise)
Stall speed: 68 km/h (36 knots, 42 mph) (with full flaps - 45º)
Range: 648 km (349 NM, 400 SM)
Service ceiling: 2440 m (8000 ft)
Rate of climb: 2.44 m/s (480 ft/min) (at maximum rate of climb and angle of climb speed of 70 mph)
Any idea if this airplane could have any market in the US?
Many Clubs are replacing now most of their AB115 with C150s and C152s, all over Brazil there are about 450 units, and seems now you can buy one for about 17K dollars..


General characteristics
Crew: 1
Capacity: 2 passengers
Length: 7.27 m (23 ft 10¼ in)
Wingspan: 10.72 m (35 ft 2 in)
Height: 2.10 m (6 ft 10½ in)
Wing area: 16.5 m² (177 ft²)
Empty weight: 530 kg (1,168 lb)
Max takeoff weight: 770 kg (1,697 lb)
Powerplant: 1× Textron Lycoming O-235-C2A four cylinder, air-cooled, horizontally-opposed, 85.5 kW (115 hp) at 2400 RPM
Performance
Maximum speed: 220 km/h (119 knots, 137 mph) at sea level
Cruise speed: 145 km/h (75 knots, 90 mph) (normal cruise)
Stall speed: 68 km/h (36 knots, 42 mph) (with full flaps - 45º)
Range: 648 km (349 NM, 400 SM)
Service ceiling: 2440 m (8000 ft)
Rate of climb: 2.44 m/s (480 ft/min) (at maximum rate of climb and angle of climb speed of 70 mph)
Any idea if this airplane could have any market in the US?